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Trying to figure out what is required to be on your panel? SO was I. In an
effort to clear the whole matter up (for me anyway) I made this page. I'll start
out by stating the FAR. (some of the items expand, if you click on the (click
to expand) thing it should open up the sub-items. Clicking it again
closes them. Pretty cool, eh?
§91.205 Powered civil aircraft with standard category U.S. airworthiness certificates: Instrument and equipment requirements.
- General. Except as provided in paragraphs (c)(3) and (e) of this section, no person may operate a powered civil aircraft with a standard category U.S. airworthiness certificate in any operation described in paragraphs (b) through (f) of this section unless that aircraft contains the instruments and equipment specified in those paragraphs (or FAA-approved equivalents) for that type of operation, and those instruments and items of equipment are in operable condition.
- Visual-flight rules (day). For VFR flight during the day, the following instruments and equipment are required:
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- Airspeed indicator.
- Altimeter.
- Magnetic direction indicator.
- Tachometer for each engine.
- Oil pressure gauge for each engine using pressure system.
- Temperature gauge for each liquid-cooled engine.
- Oil temperature gauge for each air-cooled engine.
- Manifold pressure gauge for each altitude engine.
- Fuel gauge indicating the quantity of fuel in each tank.
- Landing gear position indicator, if the aircraft has a retractable landing gear.
- For small civil airplanes certificated after March 11, 1996, in accordance with part 23 of this chapter, an approved aviation red or aviation white anticollision light system. In the event of failure of any light of the anticollision light system, operation of the aircraft may continue to a location where repairs or replacement can be made.
- If the aircraft is operated for hire over water and beyond power-off gliding distance from shore, approved flotation gear readily available to each occupant and at least one pyrotechnic signaling device. As used in this section, "shore" means that area of the land adjacent to the water which is above the high water mark and excludes land areas which are intermittently under water.
- An approved safety belt with an approved metal-to-metal latching device for each occupant 2 years of age or older.
- For small civil airplanes manufactured after July 18, 1978, an approved shoulder harness for each front seat. The shoulder harness must be designed to protect the occupant from serious head injury when the occupant experiences the ultimate inertia forces specified in §23.561(b)(2) of this chapter. Each shoulder harness installed at a flight crewmember station must permit the crewmember, when seated and with the safety belt and shoulder harness fastened, to perform all functions necessary for flight operations. For purposes of this paragraph --
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- The date of manufacture of an airplane is the date the inspection acceptance records reflect that the airplane is complete and meets the FAA-approved type design data; and
- A front seat is a seat located at a flight crewmember station or any seat located alongside such a seat.
- An emergency locator transmitter, if required by §91.207.
- For normal, utility, and acrobatic category airplanes with a seating configuration, excluding pilot seats, of 9 or less, manufactured after December 12, 1986, a shoulder harness for --
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- Each front seat that meets the requirements of §23.785 (g) and (h) of this chapter in effect on December 12, 1985;
- Each additional seat that meets the requirements of §23.785(g) of this chapter in effect on December 12, 1985.
- For rotorcraft manufactured after September 16, 1992, a shoulder harness for each seat that meets the requirements of §27.2 or §29.2 of this chapter in effect on September 16, 1991.
- Visual flight rules (night). For VFR flight at night, the following instruments and equipment are required:
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- Instruments and equipment specified in paragraph (b) of this section.
- Approved position lights.
- An approved aviation red or aviation white anticollision light system on all U.S.-registered civil aircraft. Anticollision light systems initially installed after August 11, 1971, on aircraft for which a type certificate was issued or applied for before August 11, 1971, must at least meet the anticollision light standards of part 23, 25, 27, or 29 of this chapter, as applicable, that were in effect on August 10, 1971, except that the color may be either aviation red or aviation white. In the event of failure of any light of the anticollision light system, operations with the aircraft may be continued to a stop where repairs or replacement can be made.
- If the aircraft is operated for hire, one electric landing light.
- An adequate source of electrical energy for all installed electrical and radio equipment.
- One spare set of fuses, or three spare fuses of each kind required, that are accessible to the pilot in flight.
- Instrument flight rules. For IFR flight, the following instruments and equipment are required:
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- Instruments and equipment specified in paragraph (b) of this section, and, for night flight, instruments and equipment specified in paragraph (c) of this section.
- Two-way radio communications system and navigational equipment appropriate to the ground facilities to be used.
- Gyroscopic rate-of-turn indicator, except on the following aircraft:
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- Airplanes with a third attitude instrument system usable through flight attitudes of 360 degrees of pitch and roll and installed in accordance with the instrument requirements prescribed in §121.305(j) of this chapter; and
- Rotorcraft with a third attitude instrument system usable through flight attitudes of ±80 degrees of pitch and ±120 degrees of roll and installed in accordance with §29.1303(g) of this chapter.
- Slip-skid indicator.
- Sensitive altimeter adjustable for barometric pressure.
- A clock displaying hours, minutes, and seconds with a sweep-second pointer or digital presentation.
- Generator or alternator of adequate capacity.
- Gyroscopic pitch and bank indicator (artificial horizon).
- Gyroscopic direction indicator (directional gyro or equivalent).
- Flight at and above 24,000 ft. MSL (FL 240). If VOR navigational equipment is required under paragraph (d)(2) of this section, no person may operate a U.S.-registered civil aircraft within the 50 states and the District of Columbia at or above FL 240 unless that aircraft is equipped with approved distance measuring equipment (DME). When DME required by this paragraph fails at and above FL 240, the pilot in command of the aircraft shall notify ATC immediately, and then may continue operations at and above FL 240 to the next airport of intended landing at which repairs or replacement of the equipment can be made.
- Category II operations. The requirements for Category II operations are the instruments and equipment specified in --
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- Paragraph (d) of this section; and
- Appendix A to this part.
- Category III operations. The instruments and equipment required for Category III operations are specified in paragraph (d) of this section.
- Exclusions. Paragraphs (f) and (g) of this section do not apply to operations conducted by a holder of a certificate issued under part 121 or part 135 of this chapter.
[Doc. No. 18334, 54 FR 34292, Aug. 18, 1989, as amended by Amdt. 91-220, 55 FR 43310, Oct. 26, 1990; Amdt. 91-223, 56 FR 41052, Aug. 16, 1991; Amdt. 91-231, 57 FR 42672, Sept. 15, 1992; Amdt. 91-248, 61 FR 5171, Feb. 9, 1996; Amdt. 91-251, 61 FR 34560, July 2, 1996]
Huh?
Breaking it down, I've come up with the following:
VFR Day Required
- Airspeed Indicator
- Altimeter. Evidently, this means ANY altimeter, not just the adjustable,
barometric kind.
- Magnetic Direction Indicator. Ohh, an MDI. ummm wouldn't that be a
COMPASS??
- Tachometer
- Oil pressure gauge
- Water temperature gauge (Water-cooled engine)
- Oil temperature gauge (Air-cooled engine)
- Manifold pressure gauge
- Fuel gauge for each fuel tank
- Landing gear position indicator (Not needed unless you install retractable landing gear on your RV)
- Aviation anticollision lights (Red or white)
- Floatation device (Not required unless you operate over water and for hire)
- Safety belts
- Shoulder harnesses
- ELT
- more Shoulder harnesses
- even MORE Shoulder harnesses
Although not specifically stated in 91.205, you also have to have a Mode-C transponder (per 91.215) if you want fly in the National Aerospace System.
VFR Night Additional Required
- Everything for VFR Day
- Position lights
- Anticollision light
- Landing light
- Adequate source of electricity for everything
- Spare fuses
IFR Required
- Everything so far
- Two-way radio communication and navigation
- Gyroscopic rate-of-turn indicator
- Slip-skip indicator
- Adjustable Altimeter
- Clock
- Adequate electricity from alternator
- Artificial Horizon
- Directional Gyro
OK, OK, What about MY plane?
Assuming that you will have an alternator that is capable for generating adequate power. and you have a complete set of spare fuses for
everything, here's what an RV builder should be concerned with:
- Airspeed indicator that works off of the pitot tube and static ports
- Adjustable Barometric Altimeter connected to the static port
- Compass
- Tachometer connected to EACH engine. (one will suffice)
- Oil Pressure gauge.
- Water temperature gauge for all of the water-cooled among us.
- Oil temperature gauge for the air-cooled (although, I would have one even with a water-cooled engine)
- Manifold pressure gauge for each Altitude Engine. (I found out from a few
people, thanks Mel and Rob!, that an Altitude engine is one that is
supercharged or turbocharged. That explains why I couldn't find the Manifold
Pressure gauge on the C-150 that I rent!)
- Fuel gauge for each tank
- Anticollision light suitable for night operations. Safety belts with shoulder harnesses.
- ELT.
Additionally, then to operate VFR at night:
- Position lights
- Landing light. - for hire only (Note that this must be an Electric landing light, so no candles.)
Now, for IFR:
- A two-way comm radio
- A VOR Nav radio with CDI
- Gyroscopic turn-coordinator
- Clock with second-hand (or digital)
- Artificial horizon
- Directional Gyroscope.
That's it for the regs, now here's what I want to have additionally:
- Mode-C transponder
- Another comm radio
- Another NAV radio with localizer
- Audio panel
- Marker beacons
- DME
- 2-axis Autopilot
- GPS
- maybe Maybe MAYBE an ADF
- Strobes
- Taxi Light
- Landing Light
- EGT
- CHT
- Fuel Flow
Rearranging it a little:
Engine Gauges:
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Tachometer
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VFR Day
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Oil Pressure
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VFR Day
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Oil Temperature
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VFR Day - Air Cooled Engine
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Water Temperature
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VFR Day - Water Cooled Engine
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Manifold pressure
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VFR Day - Turbocharged or Supercharged engine.
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Exhaust Gas Temperature
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Not Required
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Cylinder Head Temperature
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Not Required
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Two Fuel Gauges
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VFR Day
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Fuel Flow
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Not required
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The "Six Pack"
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Airspeed Indicator
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VFR Day
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Artificial Horizon
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IFR
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Altimeter
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VFR Day
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Turn Coordinator
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IFR
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Directional Gyro
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IFR
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Vertical Speed Indicator
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Not required
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Navigation
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Mode-C transponder
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Required by 91.215
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Compass
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VFR Day
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Comm Radio #1
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IFR
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Comm Radio #2
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Not required
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Nav Radio #1 with Localizer
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Localizer N/R, Nav Radio IFR
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Nav Radio #2
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Not required
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DME
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IFR - if flying above 24,000 MSL
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Clock
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IFR
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Marker Beacon Indicator
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Not required
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2-axis Autopilot
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Not required
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GPS
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Not required
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ADF
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Not required
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Lights
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Anticollision Lights.
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VFR Day
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Position Lights
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VFR Night
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Taxi Light
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Not required
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Landing Light
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VFR Night - for hire
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Strobes
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Not required
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Miscellaneous
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Audio Panel
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Not required
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Safety Belts, Harnesses
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VFR
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Flap position indicator
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Not required
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G-Force meter
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Not required
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Throttle
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Not required unless you want the airplane to move
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Carburetor Heat
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Not required unless you have a carburetor and want the engine to keep running
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ok, now I'm just getting silly
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